Zobrazeno 1 - 10
of 10
pro vyhledávání: '"G A, Kretinin"'
Autor:
G. V. Kretinin
Publikováno v:
Baltic Region. 2:113-120
Autor:
G. V. Kretinin
Publikováno v:
Baltic Region, Vol 4, Iss 2, Pp 53-61 (2012)
Baltic Region
Baltic Region
This article focuses on the battle career of the Russian general, Ye. F. Kern, who dedicated sixty years to the service of the country. General Kern participated in most wars and military campaigns the Russian state was involved in in the last quarte
Autor:
G. V. Kretinin, I. N. Egorov
Publikováno v:
Journal of Thermal Science. 7:218-225
The aim of this paper is to discuss a method of the compromise region determination for the multistage axial flow compressor stochastic optimization problems. This method is based on the 2-D axisymmetrical mathematical model of the compressor and on
Publikováno v:
Aircraft Engineering and Aerospace Technology. 69:518-526
Discusses a new approach to solving optimal designing and control problems in aircraft gas‐turbine engine components. This approach is a combination of optimal designing problems with optimal control problems, allowing the formation of a single pro
Autor:
A I, Autenshlius, A N, Shkunov, N B, Kuznetsova, D V, Morozova, E S, Mikhaĭlova, G A, Kretinin, E S, Luk'ianova
Publikováno v:
Problemy tuberkuleza i boleznei legkikh. (2)
A relationship was studied between the response of mononuclear cells (MNC) to fetoproteins (FP) and the bronchial changes in patients with pulmonary tuberculosis. The response was evaluated by the change in the relative count of CD8+ lymphocytes afte
Publikováno v:
10th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference.
This paper presents the main capabilities of IOSO (Indirect Optimization based on Self Organization) technology algorithms, tools and software, which can be used for the optimization of complex systems and objects, including air engine and aircraft.
Publikováno v:
8th Symposium on Multidisciplinary Analysis and Optimization.
This paper discusses two approaches to solve multidisciplinary optimization problems regarding complex engineering systems. These approaches are based upon the usage of approximation techniques. They have been developed in order to reduce computing t
Publikováno v:
Volume 1: Aircraft Engine; Marine; Turbomachinery; Microturbines and Small Turbomachinery.
The typical situation when solving a problem of an aircraft engine optimization is that a researcher has several tools for effectiveness indices analysis, distinguished according to the levels of complexity and accuracy. The high-fidelity tools can b
Publikováno v:
38th Aerospace Sciences Meeting and Exhibit.
Publikováno v:
Volume 1: Aircraft Engine; Marine; Turbomachinery; Microturbines and Small Turbomachinery.
A multicriteria optimization methodology has been discussed to determine time control laws of advanced aircraft gas turbine engines of complex structure. The resulting optimum control laws ensure top improvement of several defined power plant effecti